JASC 5330
Service difficulty reports · 79,347
Reports filed under 5330 · Fuselage Main, Plate/Skin, newest first.
Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE jasc_code = '5330' ORDER BY difficulty_date DESC"
Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE jasc_code = '5330' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR DALA2020020500898Skin · damagedEVALUATION FOR POSSIBLE FCS REPAIR ON UPPER SKIN ON TAIL ON FRAME 83 BETWEEN STRINGER 4L TO STRINGER 5L, REMOVED AND REINSTALLED EXISTING REPAIR LOCATED ON TAIL ON FRAME 82 AND BTW STR 4L TO STR 5L AS PER ER/A 549159-14 REV. A AND A320 SRM 53-51-11 FIGURE 203.SDR P5CA2016081700204Skin · crackedAPU COMPARTMENT BS 2674 - 2680, WL 305 SKIN FOUND CRACKED. REPAIRED IAW RI-53-87-11493 REV A.SDR IPXA2016081507013Skin · dentedDENT IN FUSELAGE SKIN AT BS 879 BETWEEN STRINGERS 31 AND 32L. REPAIRED IAW EO MD11-5330-60945-B.SDR SIMA20160813001Skin · crackedRIGHT UPPER AFT FUSELAGE SKIN CRACKED ABOVE STR 2R AND AFT OF FRAME 75. REPAIRED RT AFT FUSELAGE SKIN AFT OF FRAME 75 ABOVE STR 2R IAW SRM 53-31-01, ITM 11, FIG 219.SDR FOTR20160813001Skin · corrodedCORROSION ON FUSELAGE SKIN AT BS 328 STRINGER 19R JUST AFT OF FWD LAV SERVICE PANEL.SDR 4AER20161014007Skin · corrodedEXTERNAL FUSELAGE SKIN FROM BS 727G TO 907 & STRINGERS 20 TO 25R HAS CORROSION.SDR 4AER20161014006Bear Strap · corrodedAFT CARGO DOOR CUTOUT BEAR STRAP HAS CORROSION.SDR ASOA2016081215333Skin · dentedMULTIPLE DENTS IN FUSELAGE SKIN, FS 589.00-FS 605.00, STR 24R-26R, MARKED. EVALUATED DENT DAMAGE AT DISCREPANT LOCATION AND FOUND OUT OF ALLOWABLE LIMITS, SRM 53-61-31-01 AND SRM 53-00-31-01, FIG 103. COMPLIED WITH ENGINEERING DISPOSITIONS STS EA 32-2016-166SDR CALA2016081500533Skin · dentedDENT REPORTED AT 37.5 INCHES AFT OF FWD ENTRY DOOR AND 9 INCHES BELOW TOP OF FWD ENTRY DOOR, DENT MEASUREMENT 3 X 1 X .05. INSPECTED AND CLEANED DAMAGE IAW SRM 53-00-01. FOUND DAMAGE TO BE IN AREA B, FIG 104 PAGE 132.SDR CALA2016081500530Skin · dentedDENT IN FUSELAGE SKIN SPANNING BETWEEN BS 375 AND 390, ACROSS LAP JOINT AT STRINGER 24R, FRAME AT BS 380 AND STRINGERS 25 & 26R. TRIMMED OUT DAMAGED SKIN AND INSTALLED REPAIR IAW ECRA 5330- 05765.SDR CALA2016081200525Skin · gougedA MINOR GOUGE AT BS 847 - 852 BETWEEN STRINGERS 2L AND 2R. REPAIRED IAW ECRA 5331-02126.SDR FDEA201608122883Skin · corrodedFUSELAGE SKIN, STA 1681.8-1701 B/T S26R-S29R HAS CORROSION AROUND CUTOUT OF LAV SERVICE PAN. ACCOMPLISHED EA F-5330-T0327322, FUSELAGE-PLATES & SKINS. AFT LAVATORY SERVICE DOOR CUTOUT SKIN REPAIR BETWEEN STA 1675-1710 AND STR 25R-S29L, THIS IS A CAT-B, REPAISDR ABXA20160811135Skin · corrodedCORROSION FOUND ON INTERNAL BS 955 SKIN. REPAIRED IAW EA 5300013-004 AND 47008ORD09. AIRCRAFT WAS GROUNDED.SDR DALA2016081706057Skin · damagedLIGHTNING STRIKE BS 604 ABOVE STRINGER 12R. BURNISHED AREA. PERFORMED HFEC INSPECTION OF BLENDED AREA IAW ERA 549836-14, REV. ORIG, SEC 1 STEP 2. NO CRACKS INDICATED. C/W STEPS 3 AND 4 OF ERA 549836-14, REV. ORIG, SEC. 1.SDR DALA2016081206004Skin · crackedAIRCRAFT SKIN HAS CRACK AT BS 1437. REPAIRED IAW PRI/ERA 549478-14.SDR DALA2016081206009Skin · damagedLIGHTNING STRIKE AT FASTENER BS 214 STRINGER 21R. REMOVED FASTENERS IAW SRM 53-00-01 REPAIR 6 SECT 2. PERFORMED HFEC IAW NDTM PART 6 51-00-01. NO DAMAGE FOUND. INSTALLED SOLID FASTENER IAW SRM 53-00-01 SECTION 2 FIG 201. RESTORED FINISH IAW SRM 51-21-00.SDR DALA2016081206008Skin · damagedLIGHTNING STRIKE BS 659 AT FASTENER JUST ABOVE STRINGER 11R. REMOVED THE DAMAGED FASTENER IAW SRM 53-00-01 SECTION II, FIG 201. BHEC INSPECTION IAW SRM 53-00-01 FIG 201, NO ITEMS FOUND. INSTALLED SOLID FASTENER, TREATED AND PAINTED IAW SRM 53-00-01 SEC. IISDR DALA2016081206007Skin · damagedLIGHTNING STRIKE BS 682 AT FASTENER STRINGER 10R. REMOVED DAMAGED FASTENER IAW SRM 53-00-01 SECTION II FIG 201. BHED INSPECTED IAW SRM 53-00-01 FIG 201. NO ITEMS. INSTALLED A SOLID FASTENER, TREATED AND PAINTED IAW SRM 53-00-01 SEC II FIG 201.SDR DALA2016081206006Skin · damagedLIGHTNINIG STRIKE BS 765 JUST ABOVE STRINGER 11R. BURNISHED AREA. .006" MATERIAL REMOVED AND FOUND WITHIN LIMITS IAW SRM 53-00-01 ALLOWABLE DAMAGE FIG 101. TREATED AND PAINTED IAW SRM 53-00-01 FIG 101.SDR NACA2016081100059Doubler · corrodedCORRODED INTERNAL DOUBLER BETWEEN STA 967 TO 996 STR 25L. REPLACED WITH MADE REPAIR PART AND MAT IDENTIFIED IAW 65-45776 REV ER. DOUBLER INSTALLED WITH NEW SKIN REF NRC 1493466 AND NRC 1493379. RII COMPLETED.SDR NACA2016081100057Skin · crackedCRACKED FASTENER HOLES AT STA 303 JUST BELOW STR 13L AND AT STR 10L, UPPER AND LOWER DOOR HINGE CUT OUTS REPAIRED IAW SR 3-3626171693. RII COMPLETED.SDR NACA2016081100056Skin · crackedSKIN FOUND CRACKED DURING NDT, BS 291 JUST ABOVE STRINGER 10R. REPAIRED IAW BOEING SR 3-3628117058.SDR NACA2016081100053Skin · crackedSKIN CRACKED BS 259.5 STRINGER 22L. REPAIRED IAW SRM 53-30-3 FIG. 49 DETAIL V REV 101.SDR NACA2016081100041Skin · crackedSKIN CRACKED AT RADIO ALTIMETER CUTOUT AT BS 410 BETWEEN STRINGERS 28L AND 28R. SKIN REPAIRED IAW SB 53-1230 FIG.10(A).SDR ASOA20160812020Skin · damagedRIGHT NOSE SKIN DAMAGED BETWEEN FRAMES 3 AND 5, STRINGERS 4 AND 9R. REMOVED AND REPLACED THE DAMAGED SKIN .SDR CALA2016081200522Skin · dentedDENT IN FUSELAGE SKIN BETWEEN BS 420 - 440, ACROSS A 10 INCH SECTION OF STRINGER 27R. REPAIRED THE SKIN AND STRINGER IAW ECRA 5330-05766.SDR NACA2016081100013Skin · corrodedCORROSION ALONG LAP SEAM OF SKIN FROM STA 947 TO STA 1016 AT STR 25L. FOUND TO BE BEYOND LIMITS, SKIN MAT IDENTIFIED IAW SRM REV 112 ITEM 34. MADE REPAIR SKIN INSTALLED IAW DRAWING 65-45776 REV D. RII COMPLETED.SDR FDEA201608112880Skin · damagedBIRD STRIKE IMPACT CAUSED DENT IN STRUCTURE APPROXIMATELY 17" AFT OF RADOME AND 8" BELOW THE LT TAT PROBE. INSPECTED IAW EA H-5310-T0327414A PERFORMED HFEC OF EXTERNAL SKIN SURFACE OF DENT. ALSO BORESCOPE INSPECTED INTERNAL STRUCTURE AT DENT AREA. COMPLIED WSDR NACA2016081100007Skin · corrodedCORROSION LAP SEAM OF SKIN AT STA 900 TO STA 1016 STR 25R. FOUND TO BE BEYOND LIMITS. SKIN REPLACED STA 907 TO STA 1016 STR 20R TO STR 25 IAW DWG 65-45778 REV G.SDR TIMA20160810013Skin · corrodedCORROSION WAS FOUND ON THE RIGHT FUSELAGE SKIN ABOVE THE SEAT SIDE SUPPORT RAIL DURING MAINTENANCE.SDR TIMA20160810012Skin · corrodedCORROSION WAS FOUND ON THE RIGHT FUSELAGE SKIN ABOVE THE SEAT SIDE SUPPORT RAIL DURING MAINTENANCE.SDR TIMA20160810011Skin · corrodedFUSELAGE BELLY SKIN, CORROSION WAS FOUND DURING MAINTENANCE.SDR BJNA20160821001Skin · crackedCRACK FOUND IN LEFT SIDE OF THE FUSELAGE SKIN, TWO INCHES FORWARD OF BS 727G, STRINGER 24L.SDR DALA2016081106030Skin · crackedFUSELAGE SKIN CRACKED AT NOSE WHEEL WELL AFT DOOR HINGE CUTOUT. REPAIRED IAW SRM 53-30-01.SDR DALA2016081106005Skin · dentedFOUND A DENT IN FUSELAGE SKIN BS 602 BETWEEN STRINGERS 17-18L. CUTOUT DAMAGED AREA IAW SRM 53-00-01 REP 3. FABRICATED A REPAIR IAW SRM 53-00-01 REP 3, ALODINED & PRIMED THE REPAIR IAW SRM 51-20-01. INTSTALLED THE REPAIR IAW SRM 53-00-01 REP 3.SDR ASOA2016081015232Skin · damagedFUSELAGE DAMAGE BETWEEN BS 1031 AND 1051 BETWEEN STRINGERS 21 - 27R. BLENDED IAW SRM 51-12-00 AND FOUND TO BE OUT OF LIMITS IAW SRM 53-61-01. T MAJOR REPAIR IAW GMM 5-3.SDR AALA20160810012Skin · crackedFUSELAGE SKIN IS CRACKED AT BS 1418 AND LONGERON 2R. REPAIRED SKIN IAW SRM 53-04-00 FIGURE 40.SDR SPUY201608100009Skin · corrodedAFT CARGO BAY INTERNAL SKIN CORRODED BS 1351 STRINGER 29R.SDR SWAA2016092007992Skin · damagedSKIN DAMAGED AT BS 927, STRINGER 19L. REPAIRED THE SKIN IAW EA.SDR SWAA2016082254984Skin · crackedSKIN CRACKED AT BS 360, BETWEEN STRINGERS 5 - 6R. REPAIRED THE SKIN IAW ER AND EA.SDR SWAA2016082254983Skin · crackedSKIN CRACKED AT BS 360, BETWEEN STRINGERS 1 - 2L. REPAIRED THE SKIN IAW SRM.SDR AALA20160809009Skin · wornFUSELAGE SKIN AT BS 1146 IS WORN ABOVE RIGHT HORIZONTAL STABILIZER LUG FITTING. REPAIRED THE SKIN IAW SRM 51-70-13-2R-3 AND EA 262500.SDR FDEA201608092849Skin · corrodedCORROSION AT LAP SEAM STRINGER 19L, BS 740 - 770. REPAIRED IAW EA F-5330-T0327352. MAJOR REPAIR.SDR DALA2016081005915Skin · crackedA CRACK WAS FOUND, 0.125 INCH IN LENGTH ON FUSELAGE SKIN BETWEEN BS 1418, LONGERON 2-3R. REPAIRED IAW ER/A 549225-14AD REV. ORIGINAL AND ETI-88-16-282.SDR FOTR20160809002Skin · dentedAIRCRAFT FUSELAGE SKIN AT BS 1701-1720 BETWEEN STRINGER 14-16L IS DENTED.SDR SPUY201608090008Skin · crackedLOWER FUSELAGE SKIN CRACKED BS 1562 - 1640, STRINGER 24L.SDR TIPR2016080926500Skin · damagedR2 DOOR UPPER HINGE CUTOUT FOUND CRACKED AND GOUGED. REPAIRED IAW SRM 52-10-02 REPAIR 1SDR DALA2017061504739Skin · puncturedFUSELAGE SKIN LEFT BS 240, STRINGER 18L PUNCTURED. REPAIR ACCOMPLISHED.SDR IXXA20170320208Skin · corrodedBS 1582, STRINGER 10R SKIN IS CORRODED. REPAIRED IAW SRM 53-00-01, REPAIR 1 AND ED 47224REA06.SDR IXXA20161007080Skin · corrodedBS 1582 AT STRINGER 10R SKIN IS CORRODED. REPAIRED IAW SRM 53-00-1 REPAIR 1 AND ENGINEERING DOCUMENT REA 47224REA06, AIRCRAFT GROUNDED.
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